Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
Latest
Satellite identification and parameters
Extended collection of information and parameters for FENGYUN 1C DEB.
Object identification
Identified? True
Debris? True
Object name: FENGYUN 1C DEB
International designator: 1999-025CEE
Object number (NORAD): 31731
Object ID (CCSDS): 31731
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.117 minutes
Inclination: 99.3141 deg
SMA: 7142.213 km
Apoapsis: 772.287 km
Periapsis: 755.869 km
RAAN: 221.0882 deg
Eccentricy: 0.0011493
Argument of periapsis: 192.757 deg
Mean anomaly: 167.3325 deg
Mean motion: 14.3831353 rev/day
Mean motion (dot): 0.00003319 rev/day2
B* drag term: 0.001106 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 12:54 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31731U 99025CEE 25186.53776642 .00003319 00000-0 11060-2 0 9998
TLE line 2: 2 31731 99.3141 221.0882 0011493 192.7570 167.3325 14.38313530935269
Live tracking on map
Real-time ground track for satellite FENGYUN 1C DEB.
Associated space launch
Chinese polar orbiting meteorological satellite
FENGYUN 1C DEB was lifted into orbit during the mission ‘Long March 4B | Feng Yun 1C’, on board a Long March 4B space rocket.
The launch took place on May 10, 1999, 1:33 a.m. from Launch Complex 7.
For more information about the launch, click the button.
Long March 4B | Feng Yun 1C
Agency: N/A
Status: Launch Successful
Launch date: May 10, 1999, 1:33 a.m. UTC
Rocket: Long March 4B
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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